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    • Year
      1906
      2018
    • Length
      13 m
      21 m
    • Height
      3 m
      5 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      1 m2
      925 m2
    • Wingspan (Beam)
      0 m
      95 m
    • Wing loading
      3 kg/m2
      829 kg/m2
    • Swept
      4 m
      10 m
    • Sweep
      25 deg
      68 deg
    • Aspect ratio
      1
      26
    • Disc area
      134 m2
      202 m2
    • Main rotor diameter
      11 m
      17 m
    • Rotor number
      1 qt
      8 qt
    • Blades per rotor
      4 qt
      5 qt
    • Disc loading
      24 kg/m2
      37 kg/m2
    • Tail rotor diameter
      2 m
      4 m
    • Empty weight
      2369 kg
      3555 kg
    • Max. takeoff weight (Gross weight)
      4064 kg
      6097 kg
    • Loaded weight
      5 kg
      242500 kg
    • Crew
      1 per.
      2 per.
    • Useful load
      26 kg
      90700 kg
    • Payload
      23 kg
      122470 kg
    • Capacity passengers
      11 per.
      17 per.
    • Hardpoints
      1 qt
      2576 qt
    • Ground Speed
      96 km/h
      1500 km/h
    • Max. Speed
      178 km/h
      268 km/h
    • Сruise Speed
      148 km/h
      224 km/h
    • Stall Speed
      40 km/h
      258 km/h
    • Landing Speed
      68 km/h
      270 km/h
    • Minimum control speed
      24 km/h
      113 km/h
    • Never exceed speed
      107 km/h
      1050 km/h
    • Fuel Capacity
      1248 l
      1872 l
    • Fuel External
      142 l
      10025 l
    • Power/mass
      0 hp/kg
      23 hp/kg
    • Thrust/weight
      0 kN/kg
      3 kN/kg
    • Afterburning thrust
      29 kN/kg
      980 kN/kg
    • Total Power
      1439 hp
      2159 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      4242 m
      6365 m
    • Static ceiling
      2632 m
      3948 m
    • Range (Ferry range)
      351 km
      527 km
    • Range PTB (Ferry range)
      720 km
      10000 km
    • Сombat radius
      277 km
      7210 km
    • Endurance
      0 h
      150 h
    • Takeoff roll
      20 m
      3200 m
    • Landing roll
      20 m
      2570 m
    • Maximum glide ratio
      7
      43
    • Load factor from
      2 G
      9 G
    • Rate of climb
      425 m/min
      639 m/min
    • Rate of sink
      36 m/min
      56 m/min
    • Time to altitude
      0 min
      105 min
    • Propellers
      1 qt
      8 qt
    • Prop diameter
      1 m
      6 m
    • Prop blade number
      1 qt
      8 qt
    • Guns
      1 qt
      18 qt
    • Bombs
      1 qt
      250 qt
    • Missiles
      1 qt
      24 qt
    • Rockets
      1 qt
      76 qt
    • Torpedoes
      1 qt
      4 qt
    • Bombs weight
      2 kg
      39000 kg
    • Rockets weight
      1 kg
      48 kg
    • Number built
      0 qt
      43000 qt
    • Price
      41 USD
      750000000 USD

Bell 212

TypeHelicopter
Company

Bell Aircraft Corporation

Geometry
Length (m)
1.9
 
17.4
88.7
Height (m)
0.6
 
3.8
50.1
Rotors
Disc area (m2)
1.4
 
168.3
460
Main rotor diameter (m)
1.2
 
14.0
62
Disc loading (kg/m2)
17.1
 
30.2
73
Tail rotor diameter (m)
0.8
 
2.6
4.9
Weights
Empty weight (kg)
8
 
2,961.7
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
5,080.2
575,000
Capacity
Crew (per.)
1
 
1
112
Capacity passengers (per.)
1
 
14
400
Speeds
Max. Speed (km/h)
25
 
223
28,165
Сruise Speed (km/h)
52
 
186
3,087
Fuel
Fuel Capacity (l)
23
 
1,560
320,000
Power
Total Power (hp)
0.4
 
1,798.9
60,000
1 powerplant
Performance
Service ceiling (m)
0.6
 
5,303.5
161,544
Static ceiling (m)
3
 
3,290
5,485
Range (Ferry range) (km)
4
 
438.9
40,700
Dynamic Performance
Rate of climb (m/min)
1.9
 
531.9
36,000
Stat
Introduction 1968

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